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Effects of Spent Cooling and Swirler Angle on a 9-Point Swirl-Venturi InjectorNo abstract available
Document ID
20150006711
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
He, Zhuohui (NASA Glenn Research Center Cleveland, OH, United States)
Tacina, K. M. (NASA Glenn Research Center Cleveland, OH, United States)
Lee, Chi-Ming (NASA Glenn Research Center Cleveland, OH, United States)
Tacina, Robert R. (NASA Glenn Research Center Cleveland, OH, United States)
Lee, Fei Phil (Woodward FST, Inc. Zeeland, MI, United States)
Date Acquired
April 24, 2015
Publication Date
May 19, 2013
Subject Category
Aircraft Design, Testing And Performance
Aircraft Propulsion And Power
Report/Patent Number
E-18859-2
Report Number: E-18859-2
Meeting Information
Meeting: US National Combustion Meeting
Location: Park City, UT
Country: United States
Start Date: May 19, 2013
End Date: May 22, 2013
Sponsors: Combustion Inst., Utah Univ.
Funding Number(s)
WBS: WBS 794072.02.03.05.02
Distribution Limits
Public
Copyright
Public Use Permitted.

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